# Service difficulty reports: N156UP

A list on [N156UP](https://openairdocs.org/aircraft/N156UP.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 5 · 220 reports

- [SDR IPXA2026062250751](https://openairdocs.org/sdr/IPXA2026062250751.md): Skin · gouged · Jun 19, 2026 · N156UP · Airbus A300F4622R · Fuselage Main, Plate/Skin
  > MAJOR REPAIR, GOUGE ON UNDERSIDE OF TAIL SECTION LOCATED NEAR FR 83, STR 44R. ACCOMPLISHED UT PER NTM 51-10-04 LOWEST MIN IS 0.056, ACCOMPLISHED HFEC SURFACE SCAN OF REPAIRED AREA IAW NTM 51-10-08. NO CRACKS DETECTED AT THIS TIME.
- [SDR IPXA2026060994436](https://openairdocs.org/sdr/IPXA2026060994436.md): Keelbeam · cracked · May 8, 2026 · N156UP · Airbus A300F4622R · Fuselage Main, Keel
  > CRACK FOUND IN LOWER FWD HOLE OF LH SIDE OF KEEL BEAM (HOLE MARKED IN RED). ACCOMPLISH THE REPAIR PER EO-97661-REQ1 - EA 300-5312-27-A4490, REV. _.
- [SDR IPXA2026060994859](https://openairdocs.org/sdr/IPXA2026060994859.md): Keelbeam · cracked · May 8, 2026 · N156UP · Airbus A300F4622R · Fuselage Main, Keel
  > CRACK FOUND ON KEEL BEAM LH SIDE BREAK LINE AFT SIDE GOING DOWN TO UPPER AFT FASTENER. ACCOMPLISH THE REPAIR PER EO-97661-REQ1 AND EA 300-5312-27-A4490, REV. _.
- [SDR IPXA2026060995290](https://openairdocs.org/sdr/IPXA2026060995290.md): Stiffener · cracked · May 8, 2026 · N156UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > CRACK FOUND ON KEEL BEAM RH SIDE UPPER SIDE OF LOWER STIFFENER BETWEEN FR 13A AND FR 14. (AREA MARKED IN RED). ACCOMPLISHED THE REPAIR PER EO-97662-REQ1 AND EA 300-5312-27-A4491, REV. _.
- [SDR IPXA2026052633701](https://openairdocs.org/sdr/IPXA2026052633701.md): Rib · cracked · May 5, 2026 · N156UP · Airbus A300F4622R · Nacelle/Pylon, Frame/Spar/Rib
  > LEFT PYLON, RIB 3 A, PANEL FRAME WITH CRACK APPROX 1 INCHE LONG. INSTALLED RIB 3A PANEL FRAME ON LH PYLON I.A.W. A300 AMM 54-52-61/401.
- [SDR IPXA2026052129174](https://openairdocs.org/sdr/IPXA2026052129174.md): Bracket · broken · May 5, 2026 · N156UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT FR38.1/S38L-S40L THERE IS 2EA HARNESS STAND OFF BRACKETS BROKEN. INSTALLED 2EA BRACKETS AT FWD CARGO COMPARTMENT FR38.1/S38L-S40LIAW SRM 51-40-21-001.
- [SDR IPXA2026051509682](https://openairdocs.org/sdr/IPXA2026051509682.md): Rub Strip · out of limits · May 4, 2026 · N156UP · Airbus A300F4622R · Engine Thrust Reverser
  > NR 2 ENG I/B T/R AFT UPPER RUB STRIP IS GOUGED. 33-010 INSTALLED NEW RUBSTRIP AT #2 ENG I/B T/R AFT UPPER IAW A300-600 P&W SRM 54-04-01 AND STEP #7 THE SREO-51742-REQ001
- [SDR IPXA2026051115829](https://openairdocs.org/sdr/IPXA2026051115829.md): Angle · cracked · May 4, 2026 · N156UP · Airbus A300F4622R · Passenger/Crew Doors
  > CREW DOOR AFT INTERNAL SEAL, L SHAPE ANGLE IS CRACKED. INSTALLED NEW ANGLE IAW SRM 51-40-21-001.
- [SDR IPXA2026051916239](https://openairdocs.org/sdr/IPXA2026051916239.md): Bracket · cracked · May 4, 2026 · N156UP · Airbus A300F4622R · Wing Miscellaneous Structure
  > R/H WING FLAP MOVABLE FAIRING 635BB, AFT O/B ATTACH MOUNT BRACKET IS CRACKED. DOT 21-02. REMOVED AND REPLACED BRACKET P/N A5796554820300 BTCH:0004485243 AT R/H WING FLAP MOVABLE FAIRING 635BB AFT O/B IAW A300-600 SRM 51-40-21
- [SDR IPXA2026051616378](https://openairdocs.org/sdr/IPXA2026051616378.md): Panel · cracked · May 4, 2026 · N156UP · Airbus A300F4622R · Nacelle/Pylon, Main Frame
  > PYLON #1, PANEL 413BL HAS CRACKS 2(EA) AT THE GRILL DOT 31-021, PANEL STORED IN THE PANEL RACK AREA. ACCOMPLISHED WELD REPAIR ON PANEL 413BL, #1 PYLON, LOUVRE IAW A300-600 SRM 54-52-51-201 AND TRAVELER #: T26/1805003.
- [SDR IPXA2026051016492](https://openairdocs.org/sdr/IPXA2026051016492.md): Bracket · cracked · May 4, 2026 · N156UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AFT CARGO FWD BULKHEAD, SIDEWALL AT FR 54 LH UPPER CORNER BRACKET CRACKED. INSTALLED NEW BRACKET (1EA) AT AFT CARGO- FR 54 I.A.W. A300-600 SRM 51-40-21.
- [SDR IPXA2026051016514](https://openairdocs.org/sdr/IPXA2026051016514.md): Bracket · cracked · May 4, 2026 · N156UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > FAULT-STR-Z100, AFT CARGO FWD BULKHEAD, SIDEWALL AT FR 54 RH UPPER CORNER BRACKET CRACKED DOT 31-041. INSTALLED NEW BRACKET (1EA) AT AFT CARGO- FR 54 I.A.W. A300-600 SRM 51-40-21. REVIEWED
- [SDR IPXA2026060903170](https://openairdocs.org/sdr/IPXA2026060903170.md): Bulkhead · cracked · May 3, 2026 · N156UP · Airbus A300F4622R · Nacelle/Pylon, Bulkhead/Firewall
  > NR 1 ENG, INLET INTAKE, AFT BULKHEAD AT 3 O'CLOCK POSITION WITH CRACK APPROX 2 INCHES LONG. INSTALLED NEW WEB IN ZONE 400 NR 1 ENG, INLET INTAKE, AFT BULKHEAD AT 3 O'CLOCK POSITION. IAW SRM 54-10-00 REPAIR NR 14, PAGE 201, AND SRM 51-40-21-001.
- [SDR IPXA2026051002662](https://openairdocs.org/sdr/IPXA2026051002662.md): Floor Support · broken · May 3, 2026 · N156UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AVIONICS COMPARTMENT RH SIDE AT FR 10 AND FLOOR SUPPORT Y-679 ANGLE BRACKET CRACKED. INSTALLED NEW WEB P/N: A53611977200 AT AVIONICS COMPARTMENT RH SIDE AT FR 10 AND FLOOR SUPPORT Y-679 I.A.W. SRM 51-40-21.
- [SDR IPXA2026060903366](https://openairdocs.org/sdr/IPXA2026060903366.md): Sleeve · cracked · May 3, 2026 · N156UP · Airbus A300F4622R · Engine Thrust Reverser
  > NR 1 ENG, I/B T/R, TRANSLATING SLEEVE, LWR CENTER AREA, INTERNAL STRUCTURE, WITH A CRACK APPROX 3 INCHES LONG. INSTALLED ENG #1 I/B TRANSLATING SLEEVE ASSY IAW AMM A300 78-32-11/401 STEP 3C (1) THRU 3C (11)
- [SDR IPXA2026051502940](https://openairdocs.org/sdr/IPXA2026051502940.md): Rub Strip · gouged · May 3, 2026 · N156UP · Airbus A300F4622R · Engine Thrust Reverser
  > NR 2 ENG O/B T/R UPPER AFT RUB STRIP IS GOUGED. REMOVED RUBSTRIP WITH DAMAGES AT ENG #2, O/B T/R IAW P&W SRM 54-04-01. INSTALLED NEW RUBSTRIP #2 ENG O/B T/R UPPER AFT IAW SRM 54-04-01 AND STEP #7 THE SREO-51742-REQ001 ((APPX A) PERMANENT REPAIR.
- [SDR IPXA2026051502822](https://openairdocs.org/sdr/IPXA2026051502822.md): Rub Strip · gouged · May 3, 2026 · N156UP · Airbus A300F4622R · Engine Thrust Reverser
  > NR 1 ENG, O/B T/R, UPPER CENTER AREA, METAL STRIP WITH WEAR IN DIFFERENT AREAS. INSTALLED NEW RUBSTRIP IAW SRM 54-04-01,
- [SDR IPXA2026051502723](https://openairdocs.org/sdr/IPXA2026051502723.md): Rub Strip · gouged · May 3, 2026 · N156UP · Airbus A300F4622R · Engine Thrust Reverser
  > NR 1 ENG, I/B T/R, UPPER CENTER AREA, METAL STRIP WITH WEAR IN DIFFERENT AREAS.INSTALLED NEW RUBSTRIP P/N: 321A-0.40SS, IAW A300-600 P&W SRM 54-04-01 REVIEWED.
- [SDR IPXA2026051090258](https://openairdocs.org/sdr/IPXA2026051090258.md): Bracket · cracked · May 2, 2026 · N156UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > FAULT- STR- ZONE 100- AFT CARGO- FR 54 RH SIDEWALL BRACKET (2EA) CRACKED. INSTALLED NEW BRACKETS (2EA) AT AFT CARGO- FR 54 RH I.A.W. A300-600 SRM 51-40-21
- [SDR IPXA2026051190253](https://openairdocs.org/sdr/IPXA2026051190253.md): Bracket · cracked · May 2, 2026 · N156UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AFT CARGO- FR 54 LH SIDEWALL BRACKET (2EA) CRACKED DOT SH 010 INSTALLED 2(EA) BRACKETS AT ZONE 100- AFT CARGO- FR 54 LH SIDEWALL. IAW A300-600 SRM 51-40-21.
- [SDR IPXA2026051184334](https://openairdocs.org/sdr/IPXA2026051184334.md): Landing · cracked · May 2, 2026 · N156UP · Airbus A300F4622R · Wing Main, Frame Structure
  > LEFT WING T/E PANEL 575DB SUPPORT STRUCTURE CRACKED. ACCOMPLISH PERMANENT REPAIR PER EO-97380-REQ1.
- [SDR IPXA2026050679318](https://openairdocs.org/sdr/IPXA2026050679318.md): Profile · cracked · May 1, 2026 · N156UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MCD FR75 RH CRACK FOUND IN THE Z-PROFILE. INSTALLED NEW Z- PROFILE. MCD FR75 RH: I.A.W. A300-600 SRM 51-40-21-001
- [SDR IPXA2026050779287](https://openairdocs.org/sdr/IPXA2026050779287.md): Tee Angle · cracked · May 1, 2026 · N156UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MCD FR80/82 RT CRACK IN THE TEE PROFILE AT THE CORNER. REMOVED TEE PROFILE CRACKED IAW0 SRM 51-40-21-001. INSTALLED NEW TEE PROFILE IAW SRM 51-40-21-001.
- [SDR IPXA2026050779288](https://openairdocs.org/sdr/IPXA2026050779288.md): Seat Track · damaged · May 1, 2026 · N156UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MCD FR80/82 Y450 SEAT TRACK BARE METAL. UF-03. INSTALLED NEW SEAT TRACK AT Z200 - MCD FR80/82 Y450, I.A.W. A300-600 SRM 53-10-16-201 (FIG 201) AND SRM 51-40-21-001.
- [SDR IPXA2026051359595](https://openairdocs.org/sdr/IPXA2026051359595.md): Rib · cracked · Apr 30, 2026 · N156UP · Airbus A300F4622R · Wing, Rib/Bulkhead
  > CRACK FOUND CENTER FLAP ON LEFT WING TOP SKIN AND RIB FLANGES BETWEEN TRACKS LOCATED AT RIB 13 CIRCLED IN RED. INSTALLED EXTERNAL PLATE (REPAIR DOUBLER) ON LH WING, CENTER FLAP, LWR SKIN BTW RIB 13 TO RIB 14 AND STGR 2.1 TO STGR 2.2 I.A.W. SRM 57-50-00-201 PAR
- [SDR IPXA2025042985095](https://openairdocs.org/sdr/IPXA2025042985095.md): Power Supply · inoperative · Apr 28, 2025 · N156UP · Airbus A300F4622R · Door Warning System
  > AUTONOMOUS STANDBY POWER SUPPLY UNIT WILL NOT TEST. CONFIGURED A/C AND PERFORMED TEST OF AUTONOMOUS STANDBY POWER UNIT IN REF TO AMM 52-73-00/501. NO FAULTS, OPS NORMAL.
- [SDR IPXA2024072620556](https://openairdocs.org/sdr/IPXA2024072620556.md): Warning Message · false indication · Jul 26, 2024 · N156UP · Airbus A300F4622R · Landing Gear Brake System
  > **ATB** HOT BRAKES CAUTION ON ECAM AFTER GEAR RETRACTION AFTER TAKEOFF. ALL TEMPS ON LEFT TRUCK WERE HIGH WITH WHEEL #2 INDICATING 330 EXTENDED GEAR AND CONTINUE CLIMB. C/W OPS AND FUNCTIONAL TEST REF MM 32-47-00-501. ALL TEST OK
- [SDR IPXA2024022785588](https://openairdocs.org/sdr/IPXA2024022785588.md): Handle · sheared · Feb 21, 2024 · N156UP · Airbus A300F4622R · Passenger/Crew Doors
  > CREW ENTRY DOOR OUTER HANDLE ASSY SHUTTER FOUND TO BE SHEARED AT ATTACHMENT POINT. VERIFIED FIT CHECK AND SAFETIES,NO FAULT AT THIS TIME REF.MM 52-21-11
- [SDR IPXA2024022185588](https://openairdocs.org/sdr/IPXA2024022185588.md): Handle · sheared · Feb 21, 2024 · N156UP · Airbus A300F4622R · Passenger/Crew Doors
  > *SDR FILED OPEN* CREW ENTRY DOOR OUTER HANDLE ASSY SHUTTER FOUND TO BE SHEARED AT ATTACHMENT POINT.
- [SDR IPXA2023110804174](https://openairdocs.org/sdr/IPXA2023110804174.md): Unknown · unknown · Nov 8, 2023 · N156UP · Airbus A300F4622R · Escape Slide
  > SLIDE LOW PRESSURE. RESTORED DMP 52-11-01-2-3 TO NORMAL CONFIG. R&R'D ESCAPE SLIDE REF A300 AMM 25-61-21/401,
- [SDR IPXA2023102668167](https://openairdocs.org/sdr/IPXA2023102668167.md): Floor Panel · broken · Oct 26, 2023 · N156UP · Airbus A300F4622R · Fuselage Floor Panel
  > FLOOR PNL 241RN, CORNER BROKEN OFF PANEL 241 RN TO BE INSTALL IN TASK CARD 531388-01-1-231. COMPLETED PER SREO A300-5320-40552-B REVIEWED
- [SDR IPXA2023102667185](https://openairdocs.org/sdr/IPXA2023102667185.md): Floor Panel · damaged · Oct 26, 2023 · N156UP · Airbus A300F4622R · Fuselage Floor Panel
  > ACCESS Z200 -MAIN CARGO FLOOR PANEL 231PH IS DAMAGED. ACCOMPLISHED WORK ON FAULT: T3F18E00316CP. REPLACED MAIN CARGO FLOOR PANEL 231 PH, P/N B5327049200000, BAT # 0004176210. PART FOUND TO BE EFFECTIVE TO AC N156 UP IAW IPC 53-13-23-15 FIG 380. REVIEWED
- [SDR IPXA2023102668439](https://openairdocs.org/sdr/IPXA2023102668439.md): Floor Panel · broken · Oct 26, 2023 · N156UP · Airbus A300F4622R · Fuselage Floor Panel
  > FLOOR PNL 241BQ BROKEN PANEL 241 BQ TO BE INSTALL IN TASK CARD 531388-01-1-231. COMPLETED PER SREO A300-5320-40552-B REVIEWED
- [SDR IPXA2023102667660](https://openairdocs.org/sdr/IPXA2023102667660.md): Floor Panel · broken · Oct 26, 2023 · N156UP · Airbus A300F4622R · Fuselage Floor Panel
  > ACCESS Z200-FLOOR PANEL 261DM CRACKED ALL THE WAY ACROSS NEAR MIDDLE OF FLOORBOARD. DOT 3-001 PANEL 261 DM TO BE INSTALL IN TASK CARD 531388-01-1-231. COMPLETED PER SREO A300-5320-40552-B
- [SDR IPXA2023102672928](https://openairdocs.org/sdr/IPXA2023102672928.md): Floor Panel · broken · Oct 26, 2023 · N156UP · Airbus A300F4622R · Fuselage Floor Panel
  > MCD FLOOR PANEL 251XJ IS CRACKED. PANEL 251 XJ TO BE INSTALL IN TASK CARD 531388-01-1-231. COMPLETED PER SREO A300-5320-40552-B REVIEWED
- [SDR IPXA2023102669275](https://openairdocs.org/sdr/IPXA2023102669275.md): Floor Panel · broken · Oct 26, 2023 · N156UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAIN CARGO FLOOR PANEL 231LJ CRACKED DOT 65-041 PANEL 231 LJ TO BE INSTALL IN TASK CARD 531388-01-1-231. COMPLETED PER SREO A300-5320-40552-B REVIEWED
- [SDR IPXA2023102486189](https://openairdocs.org/sdr/IPXA2023102486189.md): Adapter · cracked · Oct 14, 2023 · N156UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > ACCESS 1C - FR32 -Y1959 HAS DAMAGE INSTALLED FLOOR PANEL 241 KF AND SIDE ROLLER IAW SRM 51-40-21 REVIEWED
- [SDR IPXA2023101658142](https://openairdocs.org/sdr/IPXA2023101658142.md): Flap · cracked · Oct 12, 2023 · N156UP · Airbus A300F4622R · Trailing Edge Flaps
  > *SDR FILED OPEN* FAULT-575306-01-1-687- THE R/H WING CENTER FLAP HAS A CRACK (1EA) ON RIB FLANGE #26, AREA MARKED IN RED NR 298437 WORK VERIFIED. STEP 30, 31 AND 32 EA# 300-5750-27-A3372 PRELIMINARY 1. INSPECTED. MAJOR REPAIR* FAULT-575306-01-1-687- THE R/H W
- [SDR IPXA2023103087356](https://openairdocs.org/sdr/IPXA2023103087356.md): Unknown · unknown · Oct 3, 2023 · N156UP · Airbus A300F4622R · Fuselage Main, Structure
  > CLS ADAPTER AT FR 54.2 RH 0F Y0 IS CORRODED INSTALLED CLS ADAPTER AT FR 54.2 RH. IAW SRM 51-40-21. REVIEWED
- [SDR IPXA2023102486617](https://openairdocs.org/sdr/IPXA2023102486617.md): Adapter · corroded · Oct 3, 2023 · N156UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > CLS ADAPTER AT FR 54.3 RH OF Y0 HAS CORROSION INSTALLED CLS ADAPTER AT FR 54.3 RH IAW SRM 51-40-21. ADAPTER WAS ROBBED FROM N161UP REVIEWED
- [SDR IPXA2023100651929](https://openairdocs.org/sdr/IPXA2023100651929.md): Floorboard · delaminated · Oct 2, 2023 · N156UP · Airbus A300F4622R · Fuselage Floor Panel
  > ACCESS Z100 PANEL 147CF DELAMINATED DOT 048 PNL RACK, CARD NO 298488. FABBED PANEL 147CF FROM 5024N400001SS-G BATCH # 4055277 PER SREO A300-5320-57698-A. REVIEWED
- [SDR IPXA2023100651868](https://openairdocs.org/sdr/IPXA2023100651868.md): Unknown · delaminated · Oct 2, 2023 · N156UP · Airbus A300F4622R · Fuselage Structure (General)
  > ACCESS Z100 PANEL 143DF DELAMINATED AND HYD CONTAMINATION DOT 049 PNL RACK, CARD NO 298481. FABBED PANEL 143DF FROM 5024N400001SS-G BATCH # 4055277 PER SREO A300-5320-57698-A, REVIEWED
- [SDR IPXA2023100651977](https://openairdocs.org/sdr/IPXA2023100651977.md): Unknown · delaminated · Oct 2, 2023 · N156UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > ACCESS Z100 PANEL 147BF HAS HYD CONTAMINATION AND PLASTIC FILM DIS-BONDED DOT 047 PNL RACK. CARD NO 298487 FABBED PANEL 147BF FROM 5024N400001SS-G BATCH # 4055277 PER SREO A300-5320-57698-A. REVIEWED
- [SDR IPXA2023100652030](https://openairdocs.org/sdr/IPXA2023100652030.md): Access Panel · delaminated · Oct 2, 2023 · N156UP · Airbus A300F4622R · Fuselage Structure (General)
  > ACCESS Z100 PANEL 147AF DELAMINATED DOT 049. CARD NO 298489 FABBED PANEL 147AF FROM 5024N400001SS-G BATCH # 4055277 PER SREO A300-5320-57698-A. REVIEWED
- [SDR IPXA2023103127223](https://openairdocs.org/sdr/IPXA2023103127223.md): Unknown · unknown · Sep 30, 2023 · N156UP · Airbus A300F4622R · Fuselage, Door Hinge
  > PIANO HINGE HOLES #32, #33, #36, #37, #38, AND #39 IN THE MIDDLE SECTION, HAVE CORROSION / DAMAGE INDICATIONS INSIDE THE HOLES. ALL DISCREPANT HOLES MARKED IN RED NR 299291 COMPLIED WITH EA 300-5236-27-A3386 PRELIMINARY 3 STEP 13 AND 14 IAW SRM 51-40-50. REVIE
- [SDR IPXA2023102927416](https://openairdocs.org/sdr/IPXA2023102927416.md): Unknown · unknown · Sep 30, 2023 · N156UP · Airbus A300F4622R · Fuselage, Door Hinge
  > PIANO HINGE #27 ON THE FWD SIDE, HAS CORROSION / DAMAGE INDICATIONS INSIDE THE HOLE. DISCREPANT HOLE MARKED IN RED NR 299292 REINSTALL PIANO HINGE #27 ON THE FWD SIDE IAW SRM 51-40-21 AT MAIN CARGO DOOR, WORK COMPLETED. REVIEWED
- [SDR IPXA2023103097416](https://openairdocs.org/sdr/IPXA2023103097416.md): Unknown · unknown · Sep 30, 2023 · N156UP · Airbus A300F4622R · Fuselage, Door Hinge
  > *** SDR FILED OPEN *** FAULT - 531355-02-1-233 - PIANO HINGE #27 ON THE FWD SIDE, HAS CORROSION / DAMAGE INDICATIONS INSIDE THE HOLE. DISCREPANT HOLE MARKED IN RED NR 299292 ACCOMPLISHED EO-88565-REQ1 AND EA 300-5236-27-A3386 REV.- DOCUMENT REFERENCE: SRM 51-4
- [SDR IPXA2023102927107](https://openairdocs.org/sdr/IPXA2023102927107.md): Unknown · unknown · Sep 30, 2023 · N156UP · Airbus A300F4622R · Fuselage, Door Hinge
  > PIANO HINGE HOLES #45 #44 #43 #42 #41, AND #40 ON THE AFT SIDE, HAVE CORROSION/DAMAGE INDICATIONS INSIDE THE HOLES. DISCREPANT HOLES MARKED IN RED. NR 299290 ACCOMPLISHED EO-88565-REQ1 AND EA 300-5236-27-A3386 REV.- REVIEWED
- [SDR IPXA2023102525869](https://openairdocs.org/sdr/IPXA2023102525869.md): Floor Panel · cracked · Sep 30, 2023 · N156UP · Airbus A300F4622R · Fuselage Floor Panel
  > FAULT-ACCESS Z200 - CREW AREA FLOOR PANEL 221WF IS CRACKED INS SEVERAL PLACES. CONFIRM THE INSTALLATION TO BE DONE ON ACCESS ZONE 200 BOOK
- [SDR IPXA2023102526942](https://openairdocs.org/sdr/IPXA2023102526942.md): Floor Panel · cracked · Sep 30, 2023 · N156UP · Airbus A300F4622R · Fuselage Floor Panel
  > PANEL 231 WG CRACKED. DOT 65-043 WORK IS TO BE ACCOMPLISHED ON DOC# ACCESS10Y FOR INSTALL. CONFIRMED WORK TO BE ACCOMPLISHED ON ACCESS 200 BOOK. WORK COMPLETED REVIEWED

Next page: https://openairdocs.org/aircraft/N156UP/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N156UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N156UP/reports

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